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CAMBEREDGOTTINGENSELIG-DATABASETHIN

GOE 417A (GEW.

Cambered · 3% thick · low-to-mid Re
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PROFILEGOE 417A (GEW.
surfacecamber line
GEOMETRY · AREA METRICS
max thickness3.2% @ 3%c
max camber5.9% @ 40%c
LE radius0.11%c
area upper / chord0.0518
area lower / chord0.0246
area camber / chord0.0382
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.1453-50.42183.3330.988911.671.55620ClAngle of attack (°)
Why this curve

This is a NeuralFoil prediction from the stored profile coordinates and the selected flow condition, with AeroSandbox compressibility corrections. It is not a completed OpenFOAM calculation.

Prediction error has not been calibrated for this condition. No accuracy interval is claimed.

The compressibility correction is a low-fidelity estimate, not a resolved shock or compressible CFD solution.

Geometry fit: RMS error 0.09156% of chord; maximum error 0.4318%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
162.4
Angle at maximum lift / drag (°)
6
Minimum Cd
0.006253
Maximum Cl
1.414
Angle at maximum Cl (°)
8
Cd at zero lift
0.02101
Cm at zero angle
-0.1159
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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